| Aircraft Dynamics Model
| off
| Elevator Deflection d (deg)
Vertical Gust wGust (ft/sec)
Rotary Gust qGust (rad/sec)
Gain3
Gain4
Gain5
Gain6
Sum1
Sum2
Transfer Fcn.1
Transfer Fcn.2
Vertical Velocity w (ft/sec)
Pitch Rate q (rad/sec)
|
| Controller
| off
| Stick Input (in)
alpha (rad)
q (rad/sec)
Alpha-sensor Low-pass Filter
Gain
Gain2
Gain3
Pitch Rate Lead Filter
Proportional plus integral compensator
Stick Prefilter
Sum
Sum1
Sum2
Elevator Command (deg)
|
| Dryden Wind Gust Models
| off
| Band-Limited White Noise
Q-gust model
W-gust model
Wg
Qg
|
| f14
| N/A
| u
Actuator Model
Aircraft Dynamics Model
Angle of Attack
Controller
Dryden Wind Gust Models
Gain
Gain1
Gain2
Gain5
More Info
More Info1
Nz pilot calculation
Pilot
Pilot G force Scope
Stick Input
Sum
Sum1
alpha (rad)
Nz Pilot (g)
|
| More Info
| on
|
|
| More Info1
| on
|
|
| Nz pilot calculation
| off
| w
q
Constant
Derivative
Derivative1
Gain1
Gain2
Product
Sum1
Pilot g force (g)
|
